CONNECTION,FLEXIBLE

CONTACT INFORMATION|4|N743.3|WVQ|+1 (555) 000-0000|contact@example.gov| ITEM UNIQUE IDENTIFICATION AND VALUATION (JAN 2023)|19|||||||||||||||||||| MARKINGS LEVEL I/SUBSAFE/DSS-SOC/TRIPER|5|X||||| HIGHER-LEVEL CONTRACT QUALITY REQUIREMENT (NAVICP REVIEW FEB 1991)(FEB 1999)|1|See specification sections C and E| INSPECTION OF SUPPLIES--FIXED-PRICE (AUG 1996)|2||| INSPECTION AND ACCEPTANCE - SHORT VERSION|8|X||X|||||| INSPECTION/ACCEPTANCE POINT|6||||||| GENERAL INFORMATION-FOB-DESTINATION|1|B| WIDE AREA WORKFLOW PAYMENT INSTRUCTIONS (JAN 2023)|16|Stand-Alone Receiving Report - Certifications Combo-Receiving Report & Invoice - Material |N/A|TBD|N00104|TBD|N39040 - CERTIFICATIONS, S4306A - MATERIAL|N50286|TBD|133.2|N/A|N/A|S4306A - MATERIAL|N/A|N/A|SEE DD 1423|contact@example.gov contact@example.gov| NAVY USE OF ABILITYONE SUPPORT CONTRACTOR - RELEASE OF OFFEROR INFORMATION (3-18))|1|| EQUAL OPPORTUNITY (SEP 2016)|2||| WARRANTY OF SUPPLIES OF A NONCOMPLEX NATURE (JUNE 2003)|6|ONE YEAR FROM DATE OF DELIVERY|ONE YEAR FROM DATE OF DELIVERY||||| WARRANTY OF DATA--BASIC (MAR 2014)|2||| BUY AMERICAN --FREE TRADE AGREEMENTS--BALANCE OF PAYMENTS PROGRAM - BASIC (JAN2023))|3|||| ALTERNATE A, ANNUAL REPRESENTATIONS AND CERTIFICATIONS (NOV 2020)|13|X|X|X|||X|||||||| BUY AMERICAN-BALANCE OF PAYMENTS PROGRAM CERTIFICATE-BASIC (NOV 2014)|1|| ANNUAL REPRESENTATIONS AND CERTIFICATIONS (MAR 2023)|13|332919|750|||||||||||| NOTICE OF PRIORITY RATING FOR NATIONAL DEFENSE, EMERGENCY PERPARDENESS, AND ENRGY PROGAM USE (APRIL 2008))|2||X| 1. DD1423 Data Item A001 (Inspection and Test Plan) may be waived if already onfile at NAVSUP WSS Mechanicsburg. 2. Portsmouth NSY's DODAAC has changed from N00102 to N50286. Any reference toN00102 within this order should be updated to N50286. 3. All contractual documents (i.e. contracts, purchase orders, task orders, delivery orders, and modifications) related to the instant procurement are considered to be "issued" by the Government when copies are either deposited in the mail, transmitted by facsimile, or sent by other electronic commerce methods, such as email. The Government's acceptance of the contractor's proposal constitutes bilateral agreement to "issue" contractual documents as detailed here in. 4. The following proposed delivery schedule applies: Submission of all certification data CDRLS 20 days prior to delivery. PNSY review/acceptance of certification CDRLS 6 working days after receipt Final delivery of material (365 days) 5. Only those sources with an acceptable quality control manual are eligible for award under this solicitation. Offerors are cautioned that this procurement will not be delayed solely for the purpose of approving additional sources. 6. This is a rated order certified for national defense use, and the Contractorwill follow all the requirements of the Defense Priorities and Allocations System regulation (15 CFR 700). 7. Drawings associated with this solicitation will be made available on the SAM.gov website but will be restricted access, which needs to be approved. Once access has been requested, interested vendors should email the POC listed on the solicitation to inform them of the request. 8. Quote to be a firm fixed price for the full repair of the item. This includes the teardown, evaluation, inspection and full repair of the item to "like new" or "A" condition. See statement of work in solicitation. 9. A beyond repair (BR)/ beyond economic repair (BER) price shall also beprovided in addition to the repair price at time submission of quote. 10. Do NOT include the cost for shipping material as the government implemented shipping system or ATAC will be shipping/delivering material. 11. This contract utilizes Commercial Asset Visibility (CAV). See clause NAVSUPWSSFA25 for further details. \ 1. SCOPE 1.1 The material covered in this contract/purchase order will be used in a crucial shipboard system. The use of incorrect or defective material would create a high probability of failure resulting in serious personnel injury, loss of life, loss of vital shipboard systems, or loss of the ship itself. Therefore, the material has been designated as SPECIAL EMPHASIS material (Level I, Scope of Certification, or Quality Assured) and special control procedures are invoked to ensure receipt of correct material. 2. APPLICABLE DOCUMENTS 2.1 Order of Precedence - In the event of a conflict between the text of this contract/purchase order and the references and/or drawings cited herein, the text of this contract/purchase order must take precedence. Nothing in this contract/purchase order, however, must supersede applicable laws and regulations unless a specific exemption has been obtained. 2.2 Applicable Documents - The document(s) listed below form a part of this contract/purchase order including modifications or exclusions. 2.3 Specification Revisions - The specification revisions listed under "Docu ments References" below are the preferred revision. Older and/or newer r evisions are acceptable when listed within Contract Support Library Reference Number CSD155 in ECDS (Electric Contractor Data Submission) at: ht tps://register.nslc.navy.mil/. This is to allow Contractors to use certain acceptable older specification revisions to purge their existing stock of material certified to those older revisions or to use newer specification revisions when material is certified to newly released revisions,without requiring the submittal of waiver/deviation requests for each specification revision on every contract. Revisions of specifications reflecting editorial and/or re-approval (e.g. E2009, R2014, etc.) are considered inconsequential, but are acceptable when their revisions are listedwithin CSD155 or elsewhere within this contract. 2.3.1 "Document References" listed below must be obtained by the Contractor. Ordering information is included as an attachment to this contract/purchase order. 2.3.2 The documents and drawings listed below under DRAWING NO. are not provided with this Contract/Purchase order. DRAWING NO CAGE REV DISTR CD ;300057 27826 H B 299944 27826 G B 299948 27826 B B 299950 27826 B B 299953 27826 D B 299955 27826 A B 299952 27826 C B 300027 18444 F B 302376 27826 -- B 302375 27826 -- B 302373 27826 -- B 302374 27826 -- B; DOCUMENT REF DATA=FED-STD-H28 | | |B |190424|A| | | DOCUMENT REF DATA=FF-S-86 | | |E |910116|A| 4| | DOCUMENT REF DATA=ANSI/ASQ Z1.4 | | | |080101|A| | | DOCUMENT REF DATA=QQ-N-281 | | |D |851023|A| 2| | DOCUMENT REF DATA=QQ-N-286 | | |G |001207|A| | | DOCUMENT REF DATA=ASTM-F606 | | | |191115|A| | | DOCUMENT REF DATA=MIL-STD-792 | | |F |060519|A| | | DOCUMENT REF DATA=MIL-DTL-1222 | | |J |001208|A| | | DOCUMENT REF DATA=ASTM-E1417 | | | |130601|A| | | DOCUMENT REF DATA=ASTM-E1444 | | | |160616|A| | | DOCUMENT REF DATA=MIL-STD-2035 | | |A |950515|A| | | DOCUMENT REF DATA=ASTM-D4066 | | | |130701|A| | | DOCUMENT REF DATA=ISO_9001 | | | |081115|A| | | DOCUMENT REF DATA=ISO10012 | | | |030415|A| | | DOCUMENT REF DATA=MIL-DTL-15024 | | |G |180303|A| | | DOCUMENT REF DATA=MIL-C-15726 | | |F |911008|A| 1| | DOCUMENT REF DATA=MIL-T-16420 | | |K |880916|A| 1| | DOCUMENT REF DATA=ISO/IEC 17025 | | | |050515|A| | | DOCUMENT REF DATA=MIL-DTL-18240 | | |F |000313|A| 1| | DOCUMENT REF DATA=QPL 18240 | | |QPD|170619|A| | | DOCUMENT REF DATA=MIL-DTL-24202 | | |A |171017|A| | | DOCUMENT REF DATA=MIL-C-24679 | | | |880506|A| | | DOCUMENT REF DATA=MIL-I-45208 | | |A |810724|A| 1| | DOCUMENT REF DATA=MIL-STD-45662 | | |A |880801|A| | | DOCUMENT REF DATA=A-A-59004 | | |A |950907|A| | | DOCUMENT REF DATA=ANSI/NCSL Z540.3 | | | |130326|A| | | DOCUMENT REF DATA=0900-LP-003-8000 | | | |740701|A| |02| DOCUMENT REF DATA=AIA/NAS NASM 17828 | | |1 |130430|A| | | DOCUMENT REF DATA=AIA/NAS NASM 25027 | | |1 |121221|A| | | DOCUMENT REF DATA=S9074-AQ-GIB-010/248 | | | |950801|A| | | DOCUMENT REF DATA=T9074-AS-GIB-010/271 | | |1 |140911|A| | | DOCUMENT REF DATA=S9074-AR-GIB-010A/278 (CHG A) | | | |130214|A| | | 3. REQUIREMENTS 3.0.1 INSPECTION - Clean and determine if refurbishment is possible. At disassembly, the Contractor must record all identifying markings found on the parts of each assembly. The Contractor must maintain traceability of these markingsto each unit throughout refurbishment. 3.0.2 IDENTIFYING MARKINGS - Part must have a MIC (Material Identification and Control) code, heat/heat lot code, or unique Contractor traceability number/code that is visible on the part. See Material Traceability in paragraph 3 (Quality Assurance Provisions) of this contract for traceability requirements. The MIC code can consist of a 2, 3, or 4 letter material identifier, 4 or 5 digit Julian date, 3 digit lot serial number, and Certifying Activity Designator (CAD) which will be 1 or 2 letters; the 4 parts are normally separated by hyphens; examples: TIA-3089-30-QQ and ST-06262-506-A. 3.0.3 RE-USEABLE PARTS - - Any parts of the original assembly that are useable (replacement is not necessary), that are properly marked as identified above, and that have material certifications available may be utilized as initially supplied. Certifications arenot required to be resubmitted by the contractor. - Any parts of the original assembly that are useable (replacement is not necessary), are properly marked as identified above, but material certifications arenot available at the contractor's facility, a waiver must be submitted in accordance with Waiver/Deviation (Configuration Control) requirements specified elsewhere in the Contract. 3.0.4 NON-USEABLE PARTS - -Any parts of the original assembly that are not properly marked as identifie d above must be replaced and the required certifications must be submitted. - Any parts of the original assembly that are not usable (replacement is necessary) must be replaced and the required certifications must be submitted. 3.0.5 REFURBISHMENT - Upon completion of inspection, this item must be refurbished to be in accordance with ;Murdock Drawing 299944, Assembly 299944-400; , except as amplified or modified herein. This applies to all "Parts Requiring Certification" as identified elsewhere in this Contract/Purchase Order. 3.0.6 Additional SOW Requirements - ;N/A; 3.1 Material for Parts Requiring Certification - Quantitative chemical and mechanical analysis is required for the parts listed below unless specifically stated otherwise: Part - ;Body, item 1 and Attach Flange, item 6 on Murdock Drawing 299944; Back Flange, item 14 on Murdock Drawing 300027; Thread End, item 3 on Murdock Drawing 299953 or item 6 on Murdock Drawing 302376; Flare End, item 9, on Murdock Drawing 299953 or item 5 on Murdock Drawing 302376.; Material - ;MIL-C-15726, alloy C71500 or MIL-C-24679, alloy C71500; Part - ;Stud, item 8 on Murdock Drawing 299944; Material - ;QQ-N-281, class A; PART - ;Self-Locking Nut, item 9 on Murdock Drawing 299944; MATERIAL - QQ-N-281, class A annealed (hot finished or cold drawn) or class B cold drawn. All material must be from the same class. SELF-LOCKING ELEMENT- ASTM-D4066, Group 01, Class 1 or 2, Grade 1 Part - ;Socket Head Cap Screw, item 7 on Murdock Drawing 299944; Material - ;FF-S-86, QQ-N-286, form 2, annealed and age hardened and marked .K.. Self-Locking Element in accordance with MIL-DTL-18240.; Part - ;Elbow, item 10 on Murdock Drawing 299953 or item 1 on Murdock Drawing 302376; Material - ;MIL-T-16420, type I, composition 70/30 and in accordance with Murdock Drawing 300057 or Murdock Drawing 302375 and MIL-DTL-24202; 3.2 Testing Certification - Certifications are required for the following tests on the items listed below. Additional testing on other piece parts (if any) per applicable drawings is still required, but certifications are only required as listed below. Test - ;Dye Penetrant Inspection; Item - ;BODY, ATTACH FLANGE, BACK FLANGE, THREAD END and FLARE END; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;For MIL-C-15726 material - MIL-STD-2035 or 0900-LP-003-8000 For MIL-C-24679 forgings - MIL-C-24679; Test - ;Liquid Penetrant Inspection; Item - ;SOCKET HEAD CAP SCREW, item 7 and STUD, item 8 on Murdock Drawing 299944; Performance - T9074-AS-GIB-010/271; Sampling must be per MIL-DTL-1222 Acceptance - MIL-DTL-1222 Test - ;Dye Penetrant Inspection for Non-Magnetic Grades; Item - ;Self-Locking Nut, item 9 on Murdock Drawing 299944; Performance - T9074-AS-GIB-010/271 or ASTM-E1417/ASTM-E1444 (Method C solvent removal techniques must not be used on thread) Acceptance - ;NASM25027; Test - ;Dye Penetrant Inspection; Item - ;Elbow; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035 OR 0900-LP-003-8000; Test - ;Visual or Dye Penetrant Inspection (root layer if applicable); Item - ;Weldments; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - ;Visual and Dye Penetrant Inspection (final layer); Item - ;Weldments; Performance - ;T9074-AS-GIB-010/271; Acceptance - ;MIL-STD-2035; Test - Proof Pressure Test Item - Each Assembly Performance - ;Note 6 on Murdock Drawing 299944; Acceptance - No leakage or permanent deformation for a minimum of ;2 to 5; minutes Attribute - Annealing and Age Hardening Item - ;Socket Head Cap Screw; Performance - QQ-N-286 Test - Quality Conformance Tests Item - Self-Locking Nuts Performance - ;NASM25027; Acceptance - ;NASM25027; Attribute - Certificate of Completion Item - Self-Locking Nut Nonmetallic Insert Performance - ASTM-D4066, Group 01, Class 1 or 2, Grade 1 Attribute - Certificate of Compliance Item - Self-Locking Nuts Performance - This Certificate must state that self-locking nuts were manufactured by an approved source. Approved sources are those listed on QPL-25027 for the appropriate fastener. This QPL may also be considered as approved sources for Heavy Hex self-locking nuts. 3.3 The pressure tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For pressure tests below 100 PSIG, the pressure tolerance must be +1 PSIG/-0PSIG. For pressure tests at or above 100 PSIG up to and including 2500 PSIG, the pressure tolerance must be +2% / -0 PSIG rounded off to the nearest multiple of thesmallest graduation on an analog test pressure gauge, not to exceed 50 PSIG. 30 minutes / - 0 minutes. above 2500 PSIG, the pressure tolerance must be +2%/-0 PSIG, rounded off to the nearest multiple of the smallest graduation on an analog test pressure gauge, not to exceed 200 PSIG. The pressure test time tolerance must be as specified in the assembly drawing, detail drawing, design specification or elsewhere in this contract. Where pressure test time tolerances are not provided by drawings, specifications or specified elsewhere in this contract, the following must be used: For a test duration up to and including 1 hour, the tolerance must be +5 minutes / - 0 minutes. For a test duration of more than 1 hour up to and including 24 hours, the tolerance must be +30 minutes / - 0 minutes. For a test duration of more than 24 hours, the tolerance must be + 60 minutes/- 0 minutes. 3.4 Wedge Tensile Test Specimens (Headed fasteners) - A wedge tensile test must be conducted on a Full Size Fastener for each production lot and reported aspart of the Mechanical Properties. The required specimens for the Wedge Tensile Test must be separate fasteners from those required for the Yield Test. 3.4.1 Testing for Socket Head Cap Screws must be in accordance MIL-DTL-1222, paragraphs 4.5.2.3 and 4.5.2.3.1. 3.4.2 Testing for all other Headed Fasteners with a nominal diameter greater than 1/4-inch must be in accordance with ASTM-F606 for grades 5, 8, B7, and B16.For all other grades, the following wedge angles must be used. a. Except as specified in item c below, fasteners with a nominal diameter of 1/4-inch through 1-inch (inclusive) must be tested with a ten degree wedge. b. Except as specified in item c below, fasteners with a nominal diameter over 1-inch must be tested with a six degree wedge. c. Fasteners that are of grades 8, B7, B16, 410, 416, 416Se, 431, and 630 and are threaded within one diameter to the underside of the head must be tested as follows: Sizes 1/4 inch through 3/4 inch (inclusive) Use a six degree wedgeSizes over 3/4 inch Use a four degree wedge d. Fasteners which have passed testing with wedge angles greater than those specified should be considered acceptable. 3.4.3 For fasteners having a length less than the minimum specified in Table 1 of ASTM-F606, one "test specimen fastener" must be manufactured from each lot of fasteners and tested to represent that lot. The length of these test specimen fasteners must meet the minimum specified in table 1 of ASTM-F606 but must not exceed it by more than 1/4 inch. Test specimen fasteners must be the same type, style, and diameter as the production lot and must be manufactured from the same starting material, using the same manufacturing techniques as the production lot, and must be heat treated (if required) along with the production lot. 3.5 Recorded Dimensions - A Certification of recorded dimensions as depicted in Note 6 of Murdock Machine and Engineering Company drawing 300057 is required. Certification must include the actual measured dimensions. At the time of receipt inspection, rejection of any single piece must be cause for rejection of the entire lot. 3.6 Radiography is required on ;weldments and shall be identified to the weld joint; . 3.7 Certificate of Compliance - (SPECIAL EMPHASIS MATERIAL) The Contractor must prepare and submit a certificate of compliance certifying that the items/components furnished under this contract comply with the requirements of the procurement document, including any/all invoked specifications and drawings. 3.8 K-MONEL Fasteners - Material must be heat treated per QQ-N-286. 3.8.1 Fasteners that have been hot or cold headed or roll threaded must be solution annealed followed by age hardening subsequent to all heading and thread rolling operations. The mechanical properties on certifications must be actual properties of the annealed and age hardened material and must meet the requirements of QQ-N-286. 3.8.2 QQ-N-286 fasteners that have been headed and/or roll threaded must not beage hardened unless the material has been solution annealed subsequent to the heading and threading operations. Threads formed after the final age hardening heat treatment must be cut or ground only. 3.9 Slow Strain Rate Tensile Test Laboratories - The Slow Strain Rate Tensile Test of QQ-N-286 must be performed by one of the following laboratories: Huntington Alloys, a Special Metals Company Attn: Bill Bolenr 3200 Riverside Drive Huntington, WV 257059 Phone: +1 (555) 000-0000 FAX: +1 (555) 000-0000 Metallurgical Consultants, Inc. Attn: W. M. Buehler 4820 Caroline PO Box 88046 Houston, TX 77288-0046 Phone: +1 (555) 000-0000 FAX: +1 (555) 000-0000 Naval Surface Warfare Center, Carderock Division Attn: Eric Focht Code 614 9500 Macarthur Blvd West Bethesda, MD 20817-5700 Phone: +1 (555) 000-0000 FAX: +1 (555) 000-0000 Teledyne Allvac Attn: Dr. W. D. Cao 2020 Ashcraft Ave. Monroe, NC 28110 Phone: +1 (555) 000-0000 FAX: +1 (555) 000-0000 Westmoreland Mechanical Testing and Research Inc. Attn: Andrew Wisniewski P.O. Box 388 Youngstown, PA 15696-0388 Mannesmann Rohrenwerke Mannesmann Forschungsinstitut (MFI) Attn: Dr. Weiss Postfach 251160 47251 Duisburg Germany Phone: 011-49-0203-9993194 FAX: 011-49-0203-9994415 ThyssenKrupp VDM USA, Inc. Attn: D. C. Agarwal 11210 Steeplecrest Drive, Suite 120 Houston, TX 77065-4939 Phone: +1 (555) 000-0000 3.10 ;Lubricate O-rings and mating sealing surfaces with grease per CID A-A-50433 (Termalene No. 2). Lubricate threads with lubricant per CID A-A-59004 (Molykote P-37 paste). 3.11 Specification Change - For QQ-N-281, Class B material: 1 - Footnote 9 to Table II of QQ-N-281 does not apply. 2 - When starting material is Round Bar greater than 3" dia, the mechanical properties of Hex Bar apply. 3.12 Change Paragraph 3.2.5 of MIL-F-24202 to read: 3.2.5 All finished fittings must be furnished in the fully annealed condition. 3.2.5.1 After annealing, fittings produced from tubular stock must not exceed a maximum hardness of 51 rockwell 30T determined in the area of maximum bending or forming when manufactured in accordance with paragraph 3.2.3. 3.2.5.2 Fittings produced from bar, plate, or forgings in accordance with 3.2.4 must meet the hardness required by 3.2.5.1, except that the location for hardness tests may be any area of the finished fitting. 3.13 Changes to MIL-T-16420 Mechanical Properties (Table II): Copper Alloy Outside Tensile Yield Strength Elongation in and Temper Diameter Strength (.5% under load) 2" or 4x dia. 715 (70/30)...All.......50,000....18,000............30.0% (min) Fully Sizes Annealed 3.14 MIL-T-16420 UT Changes - Delete paragraph 3.4.3.4 and substitute: "3.4.3.4 Laminations. Tube required to meet the ultrasonic requirements specified in 3.4.3 must be examined for laminar discontinuities that present indications exceeding exploration threshold levels (20 percent for the contact method at +6 db; 30 percent for the immersion method at calibration) must be rejected." 3.14.1 In the second sentence of paragraph 4.4.7; delete "18 inch" and substitute "1 inch". In the last sentence, insert "3.4.3.4 and" before "3.8.2". 3.15 Component Identification Description (CID) - When applicable drawing(s) and/or specification(s) specify that a nameplate or identification plate is required, the CID number ( ;CID 990997139; ) must be added. When no plate is specified, an identification plate in accordance with MIL-DTL-15024, Type "C" on brass or Type "H" on aluminum must be securely attached to each assembly showing the above CID number. No assembly must be shipped without the CID number attached. 3.16 Thread Inspection Requirements - All threads on threaded parts must be inspected using appropriate inspection methods, inspection systems, and inspection gages/instruments in accordance with FED-STD-H28 series. Substitution of thecommercial equivalent inspection in accordance with ASME B1 series is acceptable. 3.16.1 System 21 of FED-STD-H28/20 must be used as a minimum inspection requirement for threads when the design drawing or design specification does not specify an inspection requirement. 3.16.2 For Navy and Shipyard drawings, system 21 of FED-STD-H28/20 may be substituted for System 22 without further Navy approval when the design drawing invokes System 22 and does not cite governing specifications that specifically require system 22. System 22 of FED-STD-H28/20 must be used when the drawing references other governing specifications that specifically require System 22, such as certain thread types of MIL-DTL-1222. 3.16.3 A written request for concurrence must be submitted when utilizing alternative measuring equipment or measuring systems not applicable to the specified inspection system. 3.17 Internal Threads - All internal threads must be formed by cutting. Cold forming of internal threads is not acceptable. 3.18 Welding or Brazing - When welding, brazing, and allied processes are required, they must be in accordance with S9074-AR-GIB-010A/278, (S9074-AQ-GIB-010/248 for brazing) by personnel and procedures qualified under S9074-AQ-GIB-010/248 for all production and repair welding and brazing. Procedures and Qualification Data must be submitted for review and approval prior to performing any welding or brazing. 3.19 Configuration Control - The Contractor must maintain the total equipment baseline configuration. For items of proprietary design, Contractor drawings showing the latest assembly configuration must be provided to the Government in electronic (C4) format. Definitions are provided elsewhere in the Contract/Purchase Order. 3.19.1 Waivers/Deviations - All waivers and deviations, regardless of significance or classification require review and approval by the Contracting Officer. Waivers and Deviations must be designated as Critical, Major, or Minor. The Contractor must provide a copy of this request to the QAR. Requests must include the information listed below. a. A complete description of the contract requirement affected and the nature of the waiver/deviation (non-conformance), including a classification of Critical, Major, or Minor. b. Number of units (and serial/lot numbers) to be delivered in this configuration. c. Any impacts to logistics support elements (such as software, manuals, spares, tools, and similar) being utilized by Government personnel or impacts to the operational use of the product. d. Information about remedial action being taken to prevent reoccurrence of the non-conformance. 3.19.2 All requests for Waivers/Deviations on NAVSUP-WSS Contracts must be submitted using the ECDS (Electronic Contractor Data Submission) system at https://register.nslc.navy.mil/ 3.19.3 ECPs - The Government will maintain configuration control and change authority for all modifications or changes affecting form, fit, function, or interface parameters of the Equipment and its sub-assemblies. The Contractor must submit an Engineering Change Proposal (ECP) for any Class I or II changes that impact the Equipment covered by this contract. ECPs must be prepared in Contractor format, and must include the following information: a. The change priority, change classification (Class I or Class II), and change justification. b. A complete description of the change to be made and the need for that change. c. A complete listing of other Configuration Items impacted by the proposed change and a description of the impact on those CIs. d. Proposed changes to documents controlled by the Government. e. Proposed serial/lot number effectivities of units to be produced in, or retrofitted to, the proposed configuration. f. Recommendations about the way a retrofit should be accomplished. g. Impacts to any logistics support elements (such as software, manuals, spares, tools, and similar) being utilized by Government personnel in support of the product. h. Impacts to the operational use of the product. i. Complete estimated life-cycle cost impact of the proposed change. j. Milestones relating to the processing and implementation of the engineering change. 3.20 Mercury Free - Mercury and mercury containing compounds must not be intentionally added or come in direct contact with hardware or supplies furnished under this contract. Mercury contamination of the material will be cause for rejection. 3.21 NAVSEA 0948-LP-045-7010 - Any applicable requirements of NAVSHIPS 4410.17,NAVSEA 0948-LP-045-7010, or 0948-045-7010 which the contractor must meet are included in this contract/purchase order. The above documents are for GovernmentUse Only. Further application of the above documents is prohibited.prohibited. 3.21.1 Marking of material with a Material Designator per the Drawing is also prohibited, with the exception of Fasteners. Fasteners must be marked with a Material Symbol/Designator as specified elsewhere in this contract. ^ QUALITY ASSURANCE REQUIREMENTS ^ 3.22 See CDRL DI-MISC-80678 (Test Certification) - A statement of tests performed, listing the pieces tested must be furnished along with a copy of the test results. Certification must include the contractor's name, address and date, quantity inspected, identified to the contract/purchase order and item number, and the Contractor's or authorized personnel's signature. Test certifications must reference the standard/specification, including the revision, to which the testing was performed and the acceptance criteria used. Test procedure numbers may also be referenced on test reports. Test reports on weldments must be identified to weld joint and layer. 3.23 See CDRLs DI-MISC-80875 (Welding Procedures) and DI-MISC-80876 (Weld Procedure Qualification Data) - When production or repair welding is required, the applicable welding procedure(s) and qualification data must be submitted for review and approval. In addition, the CONSUMED WELD METAL C of C as defined below must be submitted as part of the certification OQE package submitted by the Contractor. Note: These requirements do not apply to tack/spot welds. 3.23.1 Approval of the Contractor's qualification data must be obtained prior to performing any welding (production or repair). 3.23.2 If the Contractors qualification data has previously been approved by the Navy for other contracts, a copy of the original approval letter may be submitted along with the procedures and qualification data report to expedite the approval process. The approval letter must reference the applicable welding procedure and qualification data report identification/number. Prior approval does not guarantee acceptance for this or any future contracts. As far as practical, all procedures for the contract must be submitted at the same time. Welding procedures and qualification data must be submitted in a commercially available electronic format such as Adobe Acrobat PDF. The contractor must state the applicability of each weld procedure and qualification data submitted, citing the drawing number and pieces to be welded. (i.e. "WP-123 and QD-123 are submitted for the weld joint between pieces 1 and 2 on drawing ABC." "WP-456 and QD-456 are submitted for the hardfacing of piece 3 on drawing XYZ."). Authority for the repair of Special Repairs in castings and authority for the repair of wrought or forged material must be obtained from the Procurement Contracting Officer. This request must describe the defect; including size, depth, location, and a description of the proposed repair. This request for NAVSUP-WSS Contracts must be submitted via the Electronic Contractor Data Submission (ECDS) application. 3.23.3 Any new procedure qualification performed under this Contract will require the vendor to provide a minimum 48 hour notification to DCMA with an offer to observe the welding of the test assemblies. The 48 hour time limit may be modified upon mutual agreement between the vendor and DCMA. 3.23.4 When drawings require hard facing surface Iron content (Nickel for Monel valves) not to exceed 5%, the contractor must verify surface Iron or Nickel content by performing chemical testing as defined by the applicable drawing. The chemical test results must be submitted as part of the qualification data. 3.23.5 Qualification requirements for production hardfacing: The maximum qualified thickness for hardfacing must be twice the weld deposit thickness measured in the as-welded condition that is subjected to initial NDT (Non-Destructive Testing) and any additional drawing requirements. The minimum qualified thickness is the final machined thickness at which hardness testing, NDT, macro-etch, and any additional drawing requirements are satisfactorily performed. 3.23.6 Additional qualification requirements for production hardfacing thickness less than 1/8-inch: Macro-etch (or legible photomacrographs) must be submitted for review and show consistent, minimized dilution. All essential elements and any elements not listed in S9074-AQ-GIB-010/248 that influence dilution must be in the qualification data and weld procedure, with strict limits placed on each essential element. 3.23.7 Qualification requirements for production cladding: The maximum qualified thickness for cladding must be twice the weld deposit thickness measured in the as-welded condition that is subjected to initial NDT and any additional drawing requirements. The minimum qualified thickness is the final machined thickness at which NDT, side bends, macro-etch testing, and any additional drawing requirements are satisfactorily performed. 3.23.8 Preparation and retention of weld records is required, as specified by paragraph 4.1.3 of S9074-AR-GIB-010A/278. 3.23.9 See CDRL DI-MISC-80678 (Consumed Weld Metal) - A Certificate of Compliance is required for all weld filler me...